Accession Number:

AD0903841

Title:

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. volume 12. Vertical Tail Net Chordwise Pressure Distributions and Isobars.

Descriptive Note:

Final rept. on Task 3,

Corporate Author:

BOEING COMMERCIAL AIRPLANE CO SEATTLE WA

Report Date:

1972-07-15

Pagination or Media Count:

488.0

Abstract:

This report presents the results of wind tunnel pressure distribution measurements made on a model of the Boeing supersonic transport configuration during design of the prototype airplanes. This volume contains vertical tail net chordwise pressure distributions and isobars showing the effect of sideslip and rudder deflections.

Subject Categories:

  • Aerodynamics
  • Transport Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE